当飞机发动机在运转状态下进行除冰/防冰工作时，除冰/防冰设施和人员可以进入接近发动机的危险区域 .

THE ENGINE FIRE EXTINGUISHING SYSTEM IS SUPPLIED BY:

WHEN AN APU FIRE OCCURS ON GROUND:

THE MOVEMENTS OF THE PRIMARY FLIGHT CONTROL SURFACES ARE MANAGED BY:

THE ENGINE DRIVEN PUMPS (EDPs) NORMALLY PRESSURIZE:

THE YELLOW HYDRAULIC SYSTEM IS NORMALLY PRESSURIZED BY:

THE COMPLETE PROBE HEAT SYSTEM INCLUDES:

THE WING LEADING EDGE ANTI-ICED SECTIONS ARE:

THE ELECTRONIC INSTRUMENT SYSTEM (EIS) INCLUDE:

THE EIS COMPRISES SEVERAL SYSTEM COMPUTERS, THESE COMPUTERS ARE:

THE MAXIMUM STORAGE CAPACITY OF THE DIGITAL FLIGHT DATA RECORDER (DFDR) IS: